------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Data Set Author Creation Date Software Used Product Description ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0000 M. Bester 23-Jun-2004 N/A Various launch trajectories provided by KSC. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0001 S. Frey 03-Oct-2003 GTDS, IDL Trajectory data for THEMIS P1-P4 with instantaneous orbit maneuvers. Based on Maneuver Calculator B4. Original IDL logs: park_2006Aug21_020000_B4off22_i0_5_i1a53_i2a2_i1b20_i2b1_p1.log park_2006Aug21_020000_B4off22_i0_6_i1a53_i2a2_i1b19_i2b1_p2.log park_2006Aug21_020000_B4off22_i5_s_p3.log park_2006Aug21_020000_B4off22_i12_s5_p4.log M. Bester 03-Oct-2003 SatTrack V4.5 Shadow data for P1-P4 based on trajectory data. M. Bester 03-Oct-2003 SatTrack V4.5 Pass schedules for P1-P4 based on trajectory data. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0002 S. Frey 23-Oct-2003 GTDS, IDL Forward run for P1-P5 from release through the first tail season in 60 s steps. Original IDL state vector output files: p1_statevectsOct232003T174720.txt p2_statevectsOct232003T174720.txt p3_statevectsOct232003T174720.txt p4_statevectsOct232003T174720.txt p5_statevectsOct272003T112859.txt M. Bester 28-Oct-2003 SatTrack V4.5 Shadow data for P1-P5 based on trajectory data. M. Bester 02-Nov-2003 SatTrack V4.5 Pass schedules for P1-P5 based on trajectory data. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0003 S. Frey 29-Oct-2003 GTDS, IDL Forward run for P1-P5 from release through the first tail season in 60 s steps. Changed inclination for P1 and P2 to avoid long shadows. Optimized orbital period for P3 and P4. Original IDL state vector output files: p1_statevectsOct282003T171630.txt p2_statevectsOct282003T171630.txt p3_statevectsOct282003T171630.txt p4_statevectsOct282003T171630.txt p5_statevectsOct292003T192950.txt ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0004 S. Frey 01-Nov-2003 GTDS, IDL Forward run for P1 from October 2006 to June 2007 in 60 s steps. Forward run for P3 and P4 from release through the first tail season in 60 s steps. Changed RAAN and inclination for P1, P2 and P5 to avoid long shadows. Optimized RAAN for P3 and P4. Original IDL state vector output files: p1_statevectsNov12003T190647.txt p2_statevectsNov12003T190647.txt p3_statevectsNov12003T104554.txt p4_statevectsNov12003T104554.txt p5_statevectsNov12003T190647.txt M. Bester 03-Nov-2003 SatTrack V4.5 Shadow data for P1-P5 based on trajectory data. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0005 S. Frey 29-Jan-2004 GTDS, IDL Forward run for P1 - P5 in 60 s steps: P1: 21-Aug-2006 - 02-Jun-2007 P2: 21-Aug-2006 - 31-May-2007 P3: 21-Aug-2006 - 24-Apr-2007 P4: 21-Aug-2006 - 25-Apr-2007 P5: 21-Aug-2006 - 24-Apr-2007 All maneuvers are treated as spontaneous jumps from the initial to the target state. Original IDL state vector output files: p1_statevectsFeb22004T110543wd881_25.0000.txt p2_statevectsFeb22004T110543wd881_25.0000.txt p3_statevectsFeb22004T110543wd881_25.0000.txt p4_statevectsFeb22004T110543wd881_25.0000.txt p5_statevectsFeb22004T110543wd881_25.0000.txt M. Bester 07-Mar-2004 SatTrack V4.5 Shadow data for P1-P5 based on trajectory data. M. Bester 07-Mar-2004 SatTrack V4.5 Pass schedules for P1-P5 based on trajectory data. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0006 S. Frey 04-Apr-2004 GTDS, IDL Forward run for P1 - P5 in 60 s steps: P1: 21-Aug-2006 - 08_Aug_2007 P2: 21-Aug-2006 - 05-Aug-2007 P3: 21-Aug-2006 - 24-Apr-2007 P4: 21-Aug-2006 - 25-Apr-2007 P5: 21-Aug-2006 - 24-Apr-2007 "Duck-and-dodge" scenario. All maneuvers are treated as spontaneous jumps from the initial to the target state. Original IDL state vector output files: p1_statevectsMar292004T180750wd881_25.txt p2_statevectsMar292004T180750wd881_25.txt p3_statevectsMar292004T180750wd881_25.txt p4_statevectsMar292004T180750wd881_25.txt p5_statevectsMar292004T180750wd881_25.txt ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0007 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0008 S. Frey 11-Jun-2004 GTDS, IDL Forward run for entire mission for P1 - P5 in 60 s steps: P1: 21-Oct-2006 - 13-Jan-2009 P2: 21-Oct-2006 - 10-Jan-2009 P3: 21-Oct-2006 - 31-Dec-2008 P4: 21-Oct-2006 - 31-Dec-2008 P5: 21-Oct-2006 - 31-Dec-2008 THEMIS MCDR Version Based on KSC laumch trajectory for 21-Oct-2006, using first vector after probe release. All maneuvers are treated as spontaneous jumps from the initial to the target state. Original IDL state vector output files: p1_statevectsMay282004T194839_d1_xl.dat p1_statevectsMay282004T194839_d2ii_xl.dat p1_statevectsMay282004T194839_t1_high5_xl.dat p1_statevectsMay282004T194839_t2ii_xl.dat p2_statevectsMay282004T194839_d1_xl.dat p2_statevectsMay282004T194839_d2ii_xl.dat p2_statevectsMay282004T194839_t1_high5_xl.dat p2_statevectsMay282004T194839_t2ii_xl.dat p3_statevectsMay282004T194839_d1_xl.dat p3_statevectsMay282004T194839_d2ii_xl.dat p3_statevectsMay282004T194839_t1_high5_xl.dat p3_statevectsMay282004T194839_t2ii_xl.dat p4_statevectsMay282004T194839_d1_xl.dat p4_statevectsMay282004T194839_d2ii_xl.dat p4_statevectsMay282004T194839_t1_high5_xl.dat p4_statevectsMay282004T194839_t2ii_xl.dat p5_statevectsJun72004T141939_d1_xl.dat p5_statevectsMay282004T194839_d2iip5_xl.dat p5_statevectsJun82004T090329_t1_xl.dat p5_statevectsJun72004T141939_t2_xl.dat M. Bester 16-Jul-2004 SatTrack V4.5 Shadow data for P1-P5 based on trajectory data. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0009 S. Frey 10-Aug-2004 GTDS, IDL Forward run for tail season 2 for P1 - P5 in 60 s steps: P1: 10-Sep-2007 - 06-May-2008 P2: 15-Oct-2007 - 06-May-2008 P3: 15-Oct-2007 - 06-May-2008 P4: 15-Oct-2007 - 06-May-2008 P5: 15-Oct-2007 - 06-May-2008 All maneuvers are treated as spontaneous jumps from the initial to the target state. Original IDL state vector output files: p1_statevectsJul282004T174515_t2_v8bb_xl.dat p2_statevectsJul282004T174515_t2_v8bb_xl.dat p3_statevectsJul282004T174515_t2_v8bb_xl.dat p4_statevectsJul282004T174515_t2_v8bb_xl.dat p5_statevectsJul282004T174515_t2_v8bb_xl.dat M. Bester 12-Aug-2004 SatTrack V4.5 Shadow data for P1-P5 based on trajectory data. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0010 S. Frey 24-Feb-2005 GTDS, IDL Forward run for entire mission in 1 min steps. Original data set: Feb242005T183437, 312 deg RAAN M. Bester 01-Mar-2005 SatTrack V4.5 Shadow data for P1-P5 based on trajectory data. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0011 S. Frey 05-Dec-2005 IDL, GTDS, GMAN Forward run for tail season 1 in 30 sec and 10 min steps. D. Rummel Original data set: Dec42005T2125527, 312 deg RAAN, WD 07-Feb-2007 M. Bester 10-Jan-2006 SatTrack V4.6 TDRSS coverage analysis. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0012 S. Frey 10-Feb-2006 IDL, GTDS, GMAN Forward run for four mission seasons with finite targeting of all D. Rummel maneuvers with high time resolution during maneuvers (XXL file names) and with fixed 30 second time steps (INTERPOL file names). Original data set: Feb62006T154615, 312 deg RAAN, WD 07-Feb-2007 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0013 S. Frey 07-Mar-2006 IDL, GTDS, GMAN Forward run for four mission seasons with finite targeting of all D. Rummel maneuvers with high time resolution during maneuvers (XXL file names) and with fixed 30 second time steps (INTERPOL file names). This is the same data set as 0012, except that data in the maneuver status column was fixed. Original data set: Feb62006T154615, 312 deg RAAN, WD 07-Feb-2007 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0014 S. Frey 10-Jul-2006 IDL, GTDS, GMAN Forward run for all mission seasons including re-entry with finite D. Rummel targeting of all maneuvers with high time resolution during maneuvers (XXL file names) and with fixed 30 second time steps (INTERPOL file names) for a 19-Oct-2006 launch date. Original data set: Jul42006T080031Feb07g01Aug13g01Feb13g01_ALL_312_Aug18g ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0015 S. Frey 13-Sep-2006 IDL, GTDS, GMAN Forward run for launch and early orbit phase for a launch date of D. Rummel 19-Dec-2006. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0016 S. Frey 13-Oct-2006 IDL, GTDS, GMAN Forward run for all mission seasons (without reentry) with impulsive D. Rummel maneuvers in 60 sec time steps for a launch date of 20-Jan-2007. Original data sets: Oct102006T093105Feb0201Aug0901_LD2T1_289_Feb07 Oct102006T093105Feb0201Aug0901_D1T2_289_Feb07 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0017 S. Frey 02-Nov-2006 IDL, GTDS, GMAN Forward run from launch through coast period with finite maneuvers D. Rummel in 30 sec time steps for a launch date of 15-Feb-2007. Original data set: Sep292006T160818Feb02g01Aug10g01_t2_286_Feb10g.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0018 S. Frey 30-May-2007 IDL, GTDS, GMAN Forward run from 2007/138 through 2009/352 including finite maneuvers D. Rummel in 60 sec time steps. Original data set: May292007T170123Feb02g01Aug07g01Feb02g01__IPL_289up139_Aug13g.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0019 M. Bester 31-Aug-2007 IDL, GTDS, GMAN Predicted ephemeris for 30 days, beginning on 2007/242 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0020 S. Frey 06-Oct-2007 IDL, GTDS, GMAN Full ephemeris including finite maneuver trajectories for extended mission in 60 sec steps, starting at 2009/098 00:30:00. Based on definitive orbits as of 2007/256. Original data set: Sep142007T155654Feb02g01Aug07g01Feb04g01__IPL_289up256_Aug13g ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0021 S. Broschart 31-Oct-2007 JPL Full ephemeris including finite maneuver trajectories for ARTEMIS mission, starting on 2009/290. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0022 S. Frey 09-Nov-2007 IDL, GTDS, GMAN Full ephemeris including finite maneuver trajectories in 60 sec steps from 2007/313 06:00:00 to 2008/100 06:00:00. Original data set: Nov92007T123857__IPL_289up313_Feb02g ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0023 S. Broschart 04-Dec-2007 JPL Full ephemeris including finite maneuver trajectories for ARTEMIS mission, starting on 2009/10/17 (2009/290) and ending on 2012/04/19 (2012/099). File names containing "wATT" also include attitude states. File names containing "OEM" are trajectories converted to OEM format. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0024 S. Frey 26-Jul-2008 IDL, GTDS, GMAN Full ephemeris including finite maneuver trajectories in 60 sec steps from 2008/200 00:30:00 to 2009/120 00:29:00. Original data set: Mar32008T112750Feb02g01__IPL_289up063up200_Aug03g.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0025 S. Frey 03-Oct-2008 IDL, GTDS, GMAN Full ephemeris including finite maneuver trajectories in 60 sec for T2 and D2 from 2008/276 00:30:00 to 2009/275 00:29:00 UTC. D2 is cut short in terms of maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0026 S. Frey 17-Oct-2008 IDL, GTDS, GMAN Predictive ephemeris including finite maneuver trajectories in 5 sec for 2008/290 12:00:00 to 2009/320 12:00:00 UTC. Includes large orbit plane changes for THEMIS B and C. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0027 S. Broschart 31-Oct-2008 JPL Full ephemeris including finite maneuver trajectories for ARTEMIS mission. THEMIS B (P1): 2009/10/17 (2009/290) - 2012/10/18 (2012/292) THEMIS C (P2): 2009/10/17 (2009/290) - 2012/10/28 (2012/302) File names containing "wATT" also include attitude states. File names containing "OEM" are trajectories converted to OEM format. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0028 S. Broschart 31-Oct-2008 JPL Artemis peer review trajectory for THEMIS B and THEMIS C in SPK format. Contains impulsive translunar trajectory with finite burns for LOI. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0029 S. Frey 02-Dec-2008 MDT, GTDS, GMAN Full ephemeris including finite maneuver trajectories in 60 sec steps for T2 and D2. 2008/331 00:30:00.000 - 2009/281 00:29:00.000 Switch to D2 occurs at: 2009/098 00:30:00.000 Original data set: Mar32008T112750Feb02g01Aug03g01__IPL_289up063up244up331_Feb07g.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0030 S. Broschart 11-Dec-2008 JPL ARTEMIS P1 and P2 ORM target ephemeris in ECI TOD coordinates in ASCII column format (no attitudes) in 1 minute steps. THEMSI B (P1): 2009/10/23 (2009/296) - 2010/01/06 (2010/006) THEMIS C (P2): 2009/10/18 (2009/291) - 2010/02/28 (2010/059) ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0031 M. Bester 12-Feb-2009 MDT, SatTrack THEMIS A-E ephemeris and shadow analysis from 13-Feb-2009 (2009/042) to 01-Apr-2009 (2009/091). Based on operational ephemeris generated on 13-Feb-2009. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0032 S. Frey 19-Jun-2009 MDT THEMIS B and C ephemeris covering ORM sequences from 15-Jul-2009 (2009/196) 12:00:00 UTC to 30-Oct-2009 (2009/303) 12:00:00 UTC. Inlcudes finite burn trajectories - all in 5 sec steps. THEMIS B: ORM 1-5 THEMIS C: ORM 1-12 Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up161up168.txt.02 P2PC_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up161up168.txt.02 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0033 S. Frey 02-Jul-2009 MDT THEMIS B and C ephemeris covering ORM sequences from 02-Jul-2009 (2009/183) 12:00:00 UTC to 04-Aug-2009 (2009/216) 12:00:00 UTC. Inlcudes finite burn trajectories - all in 5 sec steps. THEMIS B: ORM 1 THEMIS C: ORM 1-3 Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up161up183.txt.01 P2PC_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up161up183.txt.01 Based on Greg Whiffen's ORM design version "V" (v20c) presented on 02-Jul-2009. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0034 S. Frey 10-Jul-2009 MDT THEMIS B and C ephemeris covering ORM sequences from 15-Jul-2009 (2009/196) 12:00:00 UTC to 15-Jan-2010 (2010/015) 12:00:00 UTC. Inlcudes finite burn trajectories - all in 5 sec steps. THEMIS B: ORM 1-5, Complete sequence without FTMs THEMIS C: ORM 1-25, Complete sequence without FTMs Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up161up188.txt.01 P2PC_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up161up188.txt.01 Based on Greg Whiffen's ORM design version "V" (v20c) presented on 02-Jul-2009. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0035 D. Cosgrove 23-Aug-2009 MDT THEMIS B and C ephemeris covering ARTEMIS mission phase from 07-Aug-2009 (2009/219) 00:00:00 UTC to 18-Oct-2012 (2012/292) 12:00:00 UTC. Includes finite burn trajectories - all in 1 min steps. P1_ARTEMIS_2009219_2012292.txt P2_ARTEMIS_2009219_2012302.txt Based on Greg Whiffen's ORM design version "V". ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0036 S. Frey 17-Jan-2010 MDT THEMIS A, D & E ephemeris covering Tail Season 3 from 01-Jan-2010 (2010/008) 01:00:00 UTC to 30-Jun-2010 (2010/181) 00:59:00 UTC in 1 min steps. Includes impulsive maneuvers. Original data files: P3PD_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up280up007_Apr15g.txt.01 P4PE_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up280up007_Apr15g.txt.01 P5PA_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up280up007_Apr15g.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0037 S. Frey 16-Feb-2010 MDT THEMIS A, D & E ephemeris covering Tail Season 3 from 16-Feb-2010 (2010/047) 01:00:00 UTC to 16-Jul-2010 (2010/197) 00:59:00 UTC in 1 min steps. Includes impulsive maneuvers. Original data files: P3PD_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up280up047_Apr15g.txt.01 P4PE_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up280up047_Apr15g.txt.01 P5PA_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01__IPL_289up063up244up063up280up047_Apr15g.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0038 D. Cosgrove 27-Aug-2010 IDL ARTEMIS P1 and P2 ephemeris covering Lissajous phase in 1 min steps. Includes impulsive station-keeping maneuvers. ARTEMIS P1: 22-Aug-2010 (2010/234) - 11-Apr-2010 (2011/101) ARTEMIS P2: 22-Aug-2010 (2010/234) - 19-Apr-2010 (2011/109) ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0039 S. Frey 01-Oct-2010 MDT THEMIS A, D & E ephemeris covering Dayside Season 3 from 29-Sep-2010 (2010/272) 12:00:00 UTC to 01-Jun-2011 (2011/152) 11:59:00 UTC in 1 min steps. Original data files: P3PD_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01t3Apr15g01__IPL_2010up272_Nov01g.txt.01 P4PE_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01t3Apr15g01__IPL_2010up272_Nov01g.txt.01 P5PA_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01t3Apr15g01__IPL_2010up272_Nov01g.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0040 S. Frey 12-Jan-2011 MDT THEMIS A, D & E ephemeris covering Tail Season 4 from 11-Jan-2011 (2011/011) 01:00:00 UTC to 11-Oct-2011 (2011/284) 00:59:00 UTC in 1 min steps. Original data files: P3PD_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01t3Apr15g01d3Nov01g01__IPL__May15g.txt.05 P4PE_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01t3Apr15g01d3Nov01g01__IPL__May15g.txt.05 P5PA_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01t3Apr15g01d3Nov01g01__IPL__May15g.txt.05 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0041 D. Cosgrove 14-Apr-2011 IDL ARTEMIS P1 and P2 ephemeris covering remainder of Lissajous phase, lunar orbit insertion and lunar orbit phase in 1 min steps. Includes impulsive station-keeping maneuvers, finite lunar orbit insertion and period reduction maneuvers. ARTEMIS P1: 14-Apr-2011 (2011/104) - 01-Jan-2013 (2013/001) ARTEMIS P2: 07-Apr-2011 (2011/097) - 01-Jan-2013 (2013/001) ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0042 S. Frey 23-May-2011 MDT THEMIS A, D & E ephemeris covering extended mission from 20-May-2011 (2011/140) 12:30:00 UTC to 01-Dec-2014 (2014/335) 00:28:00 UTC in 2 min steps. Original data files: P3PD_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01t3Apr15g01d3Nov01g01t4May15g01__IPL_2011up140_Nov30g.txt.01 P4PE_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01t3Apr15g01d3Nov01g01t4May15g01__IPL_2011up140_Nov30g.txt.01 P5PA_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01t3Apr15g01d3Nov01g01t4May15g01__IPL_2011up140_Nov30g.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0043 S. Frey 12-Aug-2011 MDT ARTEMIS P1 & P2 ephemeris covering the lunar orbit phase from 09-Aug-2011 (2011/221) 15:00:00 UTC to 01-Jan-2013 (2013/001) 14:59:00 UTC in 1 min steps. Includes finite orbit period reduction maneuvers. Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2011up221.txt.01 P2PC_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2011up221.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0044 S. Frey 22-Sep-2011 MDT ARTEMIS P1 ephemeris covering the lunar orbit phase from 21-Sep-2011 (2011/264) 15:00:00 UTC to 01-Jan-2013 (2013/001) 14:59:00 UTC in 1 min steps. ARTEMIS P2 ephemeris covering the lunar orbit phase from 21-Sep-2011 (2011/264) 15:00:00 UTC to 04-Aug-2012 (2012/217) 04:01:00 UTC in 1 min steps. Early stop due to lunar altitude less than 5 km. Includes finite orbit period reduction maneuvers. Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2011up264.txt.01 P2PC_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2011up264.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0045 S. Frey 24-Oct-2011 MDT ARTEMIS P1 ephemeris covering the lunar orbit phase from 21-Oct-2011 (2011/294) 15:00:00 UTC to 01-Jan-2013 (2013/001) 14:59:00 UTC in 1 min steps. ARTEMIS P2 ephemeris covering the lunar orbit phase from 21-Oct-2011 (2011/294) 15:00:00 UTC to 04-Aug-2012 (2012/217) 04:01:00 UTC in 1 min steps. Includes finite orbit period reduction maneuvers. Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2011up294.txt.01 P2PC_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2011up294.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0046 S. Frey 14-Nov-2011 MDT ARTEMIS P1 ephemeris covering the lunar orbit phase from 14-Nov-2011 (2011/318) 17:00:00 UTC to 01-Jan-2013 (2013/001) 16:59:00 UTC in 1 min steps. ARTEMIS P2 ephemeris covering the lunar orbit phase from 14-Nov-2011 (2011/318) 17:00:00 UTC to 03-Aug-2012 (2012/216) 22:42:00 UTC in 1 min steps. Includes finite orbit period reduction maneuvers. Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2011up318.txt.01 P2PC_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2011up318.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0047 S. Frey 25-Jan-2012 MDT ARTEMIS P1 ephemeris covering the lunar orbit phase from 24-Jan-2012 (2012/024) 15:00:00 UTC to 01-Aug-2012 (2012/214) 00:00:00 UTC in 1 min steps. ARTEMIS P2 ephemeris covering the lunar orbit phase from 24-Jan-2012 (2012/024) 15:00:00 UTC to 01-Aug-2012 (2012/214) 00:00:00 UTC in 1 min steps. Includes finite orbit period reduction maneuvers. Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2012up024.txt.01 P2PC_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2012up024.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0048 S. Frey 17-Feb-2012 MDT ARTEMIS P1 ephemeris covering the lunar orbit phase from 16-Feb-2012 (2012/047) 00:00:00 UTC to 20-Feb-2013 (2013/051) 00:00:00 UTC in 1 min steps. Includes finite orbit period reduction maneuvers. Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2012up046.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0049 J. Marchese 27-Mar-2012 MDT ARTEMIS P2 ephemeris covering the lunar orbit phase from 23-Mar-2012 (2012/083) 15:00:00 UTC to 31-Dec-2012 (2012/366) 14:55:00 UTC in 5 min steps. Includes finite maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0050 S. Frey 11-May-2012 MDT ARTEMIS P1 and P2 ephemeris covering the lunar orbit phase from 11-May-2012 (2012/132) 15:00:00 UTC to 20-Feb-2013 (2013/051) 14:49:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. Original data files: P1PB_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2012up132.txt.01 P2PC_statevecs_GMAN_Mar32008T112750Feb02g01Aug03g01Feb07g01Aug10g01orsk__IPL_2012up132.txt.01 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0051 S. Frey 28-May-2012 MDT ARTEMIS P1 and P2 ephemeris covering the lunar orbit phase from 28-Jun-2012 (2012/180) 00:00:00 UTC to 01-Mar-2013 (2013/060) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0052 S. Frey 20-Jul-2012 MDT THEMIS A,D,E ephemeris from 28-Jun-2012 (2012/180) 00:00:00 UTC to 06-Sep-2017 (2017/249) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. The source data, from 2012/179, are in the separate subdirectories of /disks/gaea/disk2/sfrey/post_t5/day5_op2/ representing the three seasons: D5: long_ephem: 2012/180 00:00:00.000 - 2014/340 00:00:00.000 T8: long_ephem2: 2014/340 00:01:00.000 - 2016/158 00:00:00.000 T9: long_ephem3: 2016/158 00:01:00.000 - 2017/249 00:00:00.000 D5 comes with the intended phasing for RBSP cooperation, whereas T8 and T9 just have the apogee raises but no particular phasing yet. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0053 S. Frey 07-Sep-2012 MDT THEMIS A,D,E ephemeris from 30-Aug-2012 (2012/243) 00:00:00 UTC to 06-Sep-2017 (2017/249) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. THEMIS B,C ephemeris from 30-Aug-2012 (2012/243) 00:00:00 UTC to 01-Sep-2013 (2013/244) 00:00:00 UTC in 1 min steps. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0054 S. Frey 08-Nov-2012 MDT THEMIS B,C ephemeris from 08-Nov-2012 (2012/313) 00:00:00 UTC to 08-Nov-2013 (2013/312) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0055 S. Frey 22-Feb-2013 MDT THEMIS A,D,E ephemeris from 21-Feb-2013 (2013/052) 00:00:00 UTC to 06-Sep-2017 (2017/249) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0056 S. Frey 21-Mar-2013 MDT THEMIS B,C (ARTEMIS P1,P2) ephemeris from 21-Mar-2013 (2013/080) 00:00:00 UTC to 01-Dec-2014 (2014/335) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0057 S. Frey 10-Jul-2013 MDT THEMIS B,C (ARTEMIS P1,P2) ephemeris from 11-Jul-2013 (2013/192) 00:00:00 UTC to 30-Dec-2014 (2014/364) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0058 S. Frey 21-Nov-2013 MDT THEMIS A,D,E ephemeris from 21-Sep-2013 (2013/325) 00:00:00 UTC to 06-Sep-2017 (2017/249) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0059 S. Frey 24-Jun-2014 MDT THEMIS B,C (ARTEMIS P1,P2) ephemeris from 19-Jun-2014 (2014/170) 00:00:00 UTC to 01-Mar-2015 (2015/060) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0060 S. Frey 06-Aug-2014 MDT THEMIS A,D,E ephemeris from 18-Jul-2014 (2014/199) 00:00:00 UTC to 31-Dec-2020 (2020/366) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0061 S. Frey 19-Aug-2014 MDT THEMIS B,C (ARTEMIS P1,P2) ephemeris from 19-Aug-2014 (2014/231) 00:00:00 UTC to 20-Aug-2016 (2016/233) 00:00:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0062 S. Frey 27-Apr-2015 MDT THEMIS A,D,E ephemeris from 27-Apr-2015 (2015/117) 00:00:00 UTC to 11-Sep-2017 (2017/254) 23:59:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0063 S. Frey 09-Oct-2015 MDT THEMIS A,D,E ephemeris from 06-Oct-2015 (2015/279) 00:00:00 UTC to 31-Dec-2020 (2020/366) 23:59:00 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0064 S. Frey 11-Nov-2016 MDT ARTEMIS P1PB and P2PC ephemeris covering the lunar orbit phase from 11-Nov-2016 (2016/313) 06:00:00 to 01-Jan-2023 (2023/001) 00:01:00 UTC in 1 min steps. No orbit adjust maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0065 S. Frey 29-Nov-2016 MDT THEMIS A,D,E ephemeris from 2016-Nov-23 (2016/328) 00:00:00 UTC to 2024-Dec-31 (2024/366) 23:59:00.000 UTC in 1 min steps. Includes finite orbit adjustment maneuvers. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0066 S. Frey 22-Feb-2018 MDT THEMIS A,D,E ephemeris from 2018-Feb-12 (2018/043) 00:00:00 UTC to 2026-Jan-01 (2026/001) 00:00:00.000 UTC in 1 min steps. Includes finite orbit adjustment maneuvers to control LT targeting in 2022 and 2023. UT targeting is set for D10 only. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0067 S. Frey 05-Jul-2018 MDT THEMIS A,D,E ephemeris from 2018-Jul-03 (2018/185) 00:00:00 UTC to 2027-May-31 (2027/151) 23:59:00.000 UTC in 1 min steps. Includes finite orbit adjustment maneuvers to control LT targeting in 2022 and 2023. UT targeting is set for D10 only. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0068 S. Frey 29-Aug-2019 MDT ARTEMIS P1PB and P2PC ephemeris covering the lunar orbit phase from 2019/240 00:00:00.000 to 2023/159 23:59:00.000 UTC in 1 min steps. No orbit adjust maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0069 S. Frey 08-Jul-2020 MDT THEMIS A,D,E ephemeris from 2020-Jul-08 (2020/190) 00:00:00 UTC to 2027-Jul-08 (2027/189) 23:59:00.000 UTC in 1 min steps. These are the final orbits with regards to LT drift and after the maneuver for D12 targeting UT in Dec. 2020. No orbit adjust maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0070 S. Frey 11-May-2021 MDT THEMIS A,D,E ephemeris from 2021-May-10 (2021/130) 00:00:00 UTC to 2028-Apr-28 (2028/118) 23:59.000 UTC in 1 min steps. These are the final orbits with regards to LT drift. No maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0071 S. Frey 11-May-2021 MDT ARTEMIS P1PB and P2PC ephemeris covering the lunar orbit phase from 2021/118 00:00:0 through 2028/118 23:59:00.000 UTC in 1 min steps. These are updates after P1 shadow reduction maneuver on 2021-Mar-22. No more maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0072 S. Frey 27-May-2022 MDT ARTEMIS P1PB and P2PC ephemeris covering the lunar orbit phase from 2022-May-25 (2022/145)00:00:00 through 2029-May-24 (2029/144) 23:59:00.000 UTC in 1 min steps. No more maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0073 S. Frey 27-May-2022 MDT THEMIS A,D,E ephemeris from 2022-May-27 (2022/147) 00:00:00 UTC to 2029-May-28 (2029/147) 00:00:00 UTC in 1 min steps. These are the final orbits with regards to LT drift. No maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0074 S. Frey 30-Dec-2022 MDT ARTEMIS P1PB and P2PC ephemeris covering the lunar orbit phase from 2022-Dec-28 (2022/362) 00:00:00 through 2026-Nov-30 (2026/334) 23:59:00.000 UTC in 1 min steps. No more maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0075 J. Marchese 14-Jun-2023 MDT THEMIS A,D,E ephemeris from 2023-Jun-14 (2023/165) 00:00:00 UTC to 2029-May-28 (2029/147) 00:00:00 UTC in 1 min steps. Post-maneuver updates for P3M1C. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0076 J. Marchese 14-Jun-2023 MDT ARTEMIS P1PB and P2PC ephemeris covering the lunar orbit phase from 2023-May-31 (2022/151) 00:00:00 through 2026-Nov-30 (2026/334) 23:59:00.000 UTC in 1 min steps. No more maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0077 J. Marchese 22-Aug-2024 MDT THEMIS A,D,E ephemeris from 2024-Aug-23 (2024/236) 00:00:00.000 UTC to 2029-Aug-21 (2029/233) 23:59:00.000 UTC in 1 min steps. Post-maneuver updates for P3M1C. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 0078 J. Marchese 6-Aug-2024 MDT ARTEMIS P1PB and P2PC ephemeris covering the lunar orbit phase from 2024-Aug-06 (2022/219) 00:00:00 to 2028-Jan-30 (2028/030 23:59:00.000 UTC in 1 min steps. No more maneuvers are planned at this time. ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------